View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 28932U 06002B 25191.33311994 .00003007 00000-0 17652-3 0 9997
2 28932 98.2152 314.0678 0057715 344.4577 15.4876 15.11231682 57778
| Epoch (UTC): | 10 July 2025 07:59:41 |
| Eccentricity: | 0.0057715 |
| inclination: | 98.2152° |
| perigee height: | 492 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 314.0678° |
| argument of perigee: | 344.4577° |
| revolutions per day: | 15.11231682 |
| mean anomaly at epoch: | 15.4876° |
| orbit number at epoch: | 5777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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